N425QS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| NetJets Aviation, Inc. (DXTA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
16 reports on file, 2011-11-02 – 2020-08-13.
Part: RELAY — DEFECTIVE (DOOR) · airframe 11,066 hrs · 5,449 cycles
MAIN ENTRY DOOR WILL NOT CLOSE USING OUTDOOR SWITCH IN NOSE PANEL. SWITCH LATCHES UP, AUX PUMP IS WORKING, BUT DOOR WILL NOT CLOSE. COCKPIT SWITCH AND INSIDE ENTRY DOOR SWITCH CLOSE DOOR NORMALLY.///SIGN-OFF///REMOVED AND REPLACED 191K1 RELAY AS PER WD 52-70-00 AND SWP CHAPTER 20. PERFORMED OPERATIONAL TEST OF THE MAIN ENTRY DOOR SYSTEM. ALL TEST SATISFACTORY.
Earlier reports · 2011–2017 · 15 reports
2017
Part: BELLCRANK — CORRODED (RT WING SPOILER) · corrosion level 3 · airframe 8,980 hrs · 4,415 cycles
RIGHT INBOARD SPOILER BELLCRANK HAS CORROSION.
Part: ROLLER — GOUGED (LT WING TE FLAP) · airframe 8,980 hrs · 4,415 cycles
LEFT FLAP A TRACK INBOARD ROLLER FITTING HAS A GOUGE .040 X .010.
Part: PANEL — GOUGED (LT WING TE FLAP) · airframe 8,980 hrs · 4,415 cycles
LEFT A FLAP TRACK HAS A CHAFED GROOVE INTO SURFACE OF FLAP WELL.
Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · corrosion level 2
RIGHT C FLAP TRACK CORRODED ON THE ROLLER SURFACES. APPROACHING MANUFACTURERS MINIMUM TOLERANCE
Part: PANEL — GOUGED (RT WING TE FLAP) · airframe 8,980 hrs · 4,415 cycles
RIGHT A FLAP TRACK HAS A CHAFED GROOVE INTO SURFACE OF FLAP WELL.
Part: BELLCRANK — CORRODED (RT WING SPOILER) · corrosion level 3 · airframe 8,980 hrs · 4,415 cycles
RIGHT OUTBOARD SPOILER BELLCRANK HAS CORROSION.
Part: BELLCRANK — CORRODED (LT WING TE FLAP) · corrosion level 3 · airframe 8,980 hrs · 4,415 cycles
LEFT INBOARD FLIGHT SPOILER BELLCRANK CORRODED.
Part: WINGLET — CORRODED (RT WING) · corrosion level 2 · airframe 8,980 hrs · 4,415 cycles
RIGHT WINGLET HAS THREE PITTED VERTICAL BORES, NR 12, 13, AND 16. REQUIRES OVERSIZE REPAIR.
Part: FLAP TRACK — CORRODED (RT WING TE FLAPS) · corrosion level 2 · airframe 8,980 hrs · 4,415 cycles
RIGHT B FLAP TRACK CORRODED ON THE ROLLER SURFACES. APPROACHING MANUFACTURERS MINIMUM TOLERANCE.
Part: FLAP TRACK — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 8,980 hrs · 4,415 cycles
LEFT C FLAP TRACK CORRODED ON ROLLER SURFACES.
Part: FLAP TRACK — CORRODED (LT WING TE FLAPS) · corrosion level 2 · airframe 8,980 hrs · 4,415 cycles
LEFT B FLAP TRACK CORRODED ON THE ROLLER SURFACES. APPROACHING MANUFACTURERS MINIMUM TOLERANCE
2015
Part: WINDSHIELD — ARCED (COCKPIT) · airframe 7,540 hrs · 3,671 cycles
DETECTED & SAW SMOKE FORM BOTTOM RT CORNER OF LT WINDSHIELD. BOTTOM RT OF WINDSHIELD HEAT HAS FAILED DUE TO ARCING. ODOR & SMOKE WENT AWAY. REMOVED AND REPLACED THE PILOT SIDE NR 1 WINDSHIELD IAW AMM 56-11-10 REVISION 10 31 2012 & CMP TASK CARD 561005 REV 10 31 2012. COMPLIED WITH ALL RT INSPECTION REQUIREMENTS IAW GMM 10 SECTION 10 4.
2012
Part: BRAKE SYS — WEAK (MLG) · airframe 4,376 hrs · 2,070 cycles
BOTH MAIN BRAKES SOFT AND SPUNGY EXCESS TRAVEL. SUGGEST CHECKING FOR AIR IN THE HYD SYS. BLED BRAKE SYS IAW MM. OPS NORMAL
2011
Part: ANTI-ICE SYSTEM — MALFUNCTIONED · airframe 4,219 hrs · 1,999 cycles
LIGHT SMOKE IN THE ENTIRE CABIN, MORE DENSE IN THE REAR PART WITH WING ANTI-ICE SWITCH TURNED ON. CABIN SIDE WALLS WERE HOT TO TOUCH. SHUTOFF WING ANTI-ICE, SMOKE CLEARED AND ODOR DISSIPATED.
Part: WHEEL — OVERHEATED (NR 1) · airframe 4,213 hrs · 1,994 cycles
NR1 OTBD MAIN WHEEL ASSY SMOKING AFTER LANDING. PEAK BRAKE TEMP WAS 102C. FLUID ALL OVER INSIDE OF TIRE. NO NOTICEABLE LEAKS OR DRIPS. SMOKING STOPPED WITHIN 15 MINUTES. RAN ENGINES AT IDLE IAW MM 72-00-00 TO PRESSURIZE BOTH HYD SYSTEMS. APPLIED BRAKES, OPENED AND CLOSED MLG DOORS, AND INSPECTED HYD LINE IN WHEEL WELL AREA AND ON THE LT MLG. NO DEFECTS FOUND. SERVICED LT & RT HYD SYS IAW MM 12-15-00 (REV 14 08/31/11).